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SpaceLoft XL : ウィキペディア英語版 | SpaceLoft XL
The SpaceLoft XL is a sounding rocket developed by private spaceflight company UP Aerospace. The rocket is capable of lofting a 110 lb (50 kg) payload to a sub-orbital trajectory with an apogee of 140 miles (225 km).〔(http://www.upaerospace.us.com )〕 It takes only 60 seconds to cross the Kármán line (the official "edge of space" at 100 km).〔(【引用サイトリンク】title=SpaceLoft™ XL )〕 Launches are conducted from the company launch facility at Spaceport America in Upham, New Mexico. ==Description== The rocket is 20 feet (6 m) long and 10 inches (25 cm) in diameter, and consists of a single stage powered by a single solid fuel rocket engine. Typical flights last about 13 minutes, with more than 4 minutes of weightlessness.〔 The rocket is reportedly capable of reaching up to 225 km (140 miles) altitude,〔(【引用サイトリンク】title=Spaceloft XL )〕 though its standard apogee is closer to 115 km.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「SpaceLoft XL」の詳細全文を読む
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